WO2015091569A1 - Bearing assembly and method - Google Patents

Bearing assembly and method Download PDF

Info

Publication number
WO2015091569A1
WO2015091569A1 PCT/EP2014/078086 EP2014078086W WO2015091569A1 WO 2015091569 A1 WO2015091569 A1 WO 2015091569A1 EP 2014078086 W EP2014078086 W EP 2014078086W WO 2015091569 A1 WO2015091569 A1 WO 2015091569A1
Authority
WO
WIPO (PCT)
Prior art keywords
section
outer race
bearing assembly
race
bearing
Prior art date
Application number
PCT/EP2014/078086
Other languages
French (fr)
Inventor
Paul PROZELLER Jr.
Original Assignee
Solvay Specialty Polymers Usa, Llc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Solvay Specialty Polymers Usa, Llc filed Critical Solvay Specialty Polymers Usa, Llc
Priority to EP14812546.1A priority Critical patent/EP3084242A1/en
Priority to US15/105,511 priority patent/US20160312830A1/en
Publication of WO2015091569A1 publication Critical patent/WO2015091569A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30Parts of ball or roller bearings
    • F16C33/58Raceways; Race rings
    • F16C33/60Raceways; Race rings divided or split, e.g. comprising two juxtaposed rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C43/00Assembling bearings
    • F16C43/04Assembling rolling-contact bearings
    • F16C43/06Placing rolling bodies in cages or bearings
    • F16C43/08Placing rolling bodies in cages or bearings by deforming the cages or the races
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2300/00Application independent of particular apparatuses
    • F16C2300/02General use or purpose, i.e. no use, purpose, special adaptation or modification indicated or a wide variety of uses mentioned

Definitions

  • Bearings may utilize bearings to support loads during the translation of motion.
  • Bearing assemblies are typically used for axial loads where 360° rotational movement is desired.
  • ball bearing materials are typically alloy steels. Steel permits high mechanical loads, long life, and resistance to wear.
  • a roller ball bearing typically consists of an inner race, an outer race, a set of ball bearings and a bearing cage. Steel bearing assemblies must be manufactured with little or no distortion of their components to avoid damage. This factor limits the number of balls that may be placed in the race, thus providing a limitation on the ultimate load bearing capability of the roller bearing assembly.
  • Metal ball bearings are constructed in such a way that all of the components are assembled in a 'static' manner.
  • the inner race is put in place on a flat surface, an outer race is placed over the top or "on" the inner race, the races are offset or spread apart to allow clearance on one side so that all of the allotted rolling elements (normally balls) may be placed in-between the two races.
  • a cage is placed over the group of ball bearings to provide and maintain equal spacing between the rolling elements.
  • Polymeric bearings are normally limited in their range of use based upon at least two factors; resilience or yield strength of the materials employed and the number of load bearing rolling elements (primarily balls) which may be incorporated for containment within the spacing between the two races.
  • the number of balls or rolling elements which can be introduced is increased by providing an elastic deformation in either or both of the two rings or races. Addition of the number of rolling elements between the races for a bearing increases the ability to support load and reduce friction and wear both external and internal to the bearing.
  • US application 2012/0047742 indicates a method for assembly of a roller bearing with the primary object of the invention being a new and improved method of assembling a rolling bearing by inserting an increased number of rolling elements between the outer and the inner rings of the rolling bearing.
  • a method for assembling a rolling bearing having an outer and an inner ring and at least one row of rolling elements there between which comprises positioning the inner ring eccentrically within the outer ring so as to form a crescent shape space.
  • the method also comprises elastic deformation of the outer ring by applying forces from outside to three points on the periphery of the outer ring.
  • Such a method allows for insertion of a greater number of rolling elements in the crescent shape space left between the inner and outer rings in an eccentric position without exceeding the elastic limit of the material constituting the outer ring.
  • the method can also be repeated after it has been ascertained that insertion of one supplemental rolling element can be made without permanently deforming the outer ring and/or the inner ring.
  • the maximum number of supplemental rolling elements which can be inserted in the crescent shape space without exceeding the elastic limit can thus be determined precisely, before applying the forces and effectively inserting the maximum number of supplemental rolling elements in said space.
  • This method can be applied to any type of rolling bearing, for example to ball bearings where the rolling elements are balls or the method can be applied to rolling bearings where the rolling elements are cylindrical rollers which could be needle bearings.
  • the rolling bearings may have more than one row of rolling elements.
  • the present application relates to both a bearing assembly and to a method for assembling a bearing.
  • the present invention provides for a bearing assembly comprising at least one, two-part non-metallic outer race, at least one inner race located within the two-part outer race having a groove along its circumferential portion, and a set of rolling elements housed between said inner race and said outer race, wherein said the two-part outer race has a first part inner section and a second part outer section,
  • both said first part inner section and said second part outer section are made from a plastic material and have individually a Morse tapered shape having a proximal end portion and a distal end portion wherein the proximal end portion have a first thickness and the distal end portion having a second thickness different from thickness of proximal end portion;
  • the bearing assembly of the present invention advantageously includes a larger number of rolling elements (balls) in the expanded volumetric space between inner and outer races than might exist for a traditional metallic bearing assembly of substantially same shape.
  • the invention additionally provides for a method for assembling the bearing assembly as above described, said method comprising;
  • FIG. 1A is a cross-sectional top or side view of a typical standard ball bearing having an inner race and an outer race.
  • FIG. IB is also a cross-sectional top or side view indicating the fabricated bearing of the present disclosure with a different outer race that has been tapered from a thicker end (from right to left) to a thinner end, resulting in the forming of a "wedge-like" taper.
  • This taper is often referred to in the literature as a "Morse” taper.
  • FIG. 2 is a detailed schematic representation of one half of a cross- sectional top side or end view of the modified outer race (OR) versus that of the conventional (OR).
  • FIG. 3 is a simple graphical representation of the "cantilever” effect showing how the thinner (OR) is more elastic at the thinner end versus that of the thicker end.
  • FIG.4 illustrates how to overcome the issues associated with the schematic shown in FIG. 3, in that the thinner outer race (OR) is reinforced by an external separate tapered element with a thinner end Tl and a thicker end T2 that is known as a Morse tapered section such that the Morse tapered section increases the thickness of the thinner outer race.
  • FIG.5 is a full cross-sectional view of a modified bearing of one
  • FIG. 6 is a full cross-sectional view of a completed bearing assembly with comparable strength and load bearing capacity to that of an unmodified bearing with an unmodified outer race.
  • the bearing assembly of the present invention generally has a symmetrical shape that is either spherical or cylindrical.
  • said two-part outer race and optionally said inner race are formed from a plastic material.
  • said two-part outer race is generally capable of at least 7 percent elongation, and according to certain embodiments even of at least 16 percent elongation, without causing an increase in the permanent yield or exceeding the elastic limit of said two-part non- metallic outer race.
  • the Morse tapered shape of the said first part inner section and said second part outer section are advantageously as defined in ISO standard 296, which is hereby incorporated by reference.
  • the said first part inner section and said second part outer section having Morse tapered shape are assembled in the bearing assembly of the invention and overlaid and bonded in step (vi) of the method as above described so that at least outer surface of said first part inner section and inner surface of said second part outer section are placed in intimate contact with one another so that there is a capability to resist slipping, disassociation (breaking apart) and essentially forming a physically single structural or load bearing unit.
  • an additional adhesive system may be used to render a more homogeneous bonded structural support.
  • This adhesive may be formulated using same plastic material which is the main constituent of said first part inner section and second part inner section.
  • the plastic material includes polymer (PAI) as polymer ingredient
  • PAI polymer
  • an acceptable solvent is NMP N-methyl pyrolidone - other solvents which at least partially solubilize polymer PAI can also be used.
  • Other bonding techniques can be used to enhance the adhesion between outer surface of said first part inner section and inner surface of said second part outer section; these techniques may include laser or spin welding, ultrasonic bonding, etc.
  • the bearing assembly of the invention may additionally comprise an additional support ring which is circumferentially fixed on the outer surface of the two-part non-metallic outer race.
  • This support ring can be machined, molded, formed or created in any suitable manner to fit with the outer surface of the two-part non-metallic outer race.
  • This support ring is generally intended to provide additional structural integrity and cause the said two-part non-metallic outer race to no longer exhibit deformable characteristics and behavior either free from or under load.
  • the plastic material of said two-part outer race and optionally of said inner race of the bearing assembly of the invention generally comprises a polymer component as major constituent and optionally one or more than one additive.
  • the plastic material of the said first part inner section and of the said second part outer section of the two-part outer race can be the same material or can be a different material. Nevertheless, embodiments wherein both said first part inner section and said second part outer section of the two-part outer race are made from the same plastic material, as detailed below.
  • polyetherarylketone polymers including PEEK
  • aromatic polyimide polymers including aromatic polyamide-imide polymer [polymer (PAI)]
  • PAI polyamide-imide polymer
  • Said additive is generally a fibrous filler selected from the group consisting of carbon fibers, molybdynum disulfide, graphite, PI PE
  • one or more non-fibrous surface modifier selected from the group consisting of a liquid, a particulate surface modifier and mixtures thereof can be further used as additives.
  • the weight percentage of these additives are to be used in combination with the polymer component could be any percentage deemed necessary to improve the physical attributes of the bearing assembly such as reduced friction and wear, toughness, and lubricity.
  • the plastic material comprises an aromatic polyamide-imide polymer [polymer (PAI)].
  • aromatic polyamide-imide polymer [polymer (PAI)] as used herein is intended to denote any polymer comprising more than 50 % moles of recurring units comprising at least one aromatic ring, at least one imide group, as such and/or in its amic acid form, and at least one amide group which is not included in the amic acid form of an imide group [recurring units (R PAI )] .
  • R PAI The recurring units (R PAI ) are advantageously chosen among those of formula :
  • Ar is a trivalent aromatic group; typically Ar is selected from the group consisting of following structures :
  • R is a divalent aromatic group; typically R is selected from the group consisting of following structures :
  • Y being -0-, -S-, -SO2-, -CH2-, -C(O)-, -C(CH 3 ) 2 -, -C(CF 3 ) 2 -, -(CF 2 ) q , q being an integer from 1 to 5.
  • the aromatic polyamide-imide comprises more than 50 % of recurring units (R PAI ) comprising an imide group in which the imide group is present as such, like in recurring units (Rp A i-a), and/or in its amic acid form, like in recurring units (Rp A i-b).
  • R PAI recurring units
  • the imide group is present as such, like in recurring units (Rp A i-a), and/or in its amic acid form, like in recurring units (Rp A i-b).
  • Recurring units are preferably chosen from recurring units (1), (m) and (n), in their amide-imide (a) or amide-amic acid (b) forms :
  • the polymer (PAI) comprises more than 90 % moles of recurring units (R PAI ). Still more preferably, it contains no recurring unit other than recurring units (R PAI ).
  • Polymers commercialized by Solvay Specialty Polymers USA, L.L.C. as TORLON ® polyamide-imides comply with this criterion.
  • Torlon ® 4000T is an aromatic polyamide-imide polymer commercially available from Solvay Specialty Polymers USA, LLC.
  • the (PAI) polymer can be manufactured according to known methods in the art.
  • the (PAI) polymer can be notably manufactured by a process including the polycondensation reaction between at least one acid monomer chosen from trimellitic anhydride and trimellitic anhydride monoacid halides and at least one comonomer chosen from diamines and diisocyanates.
  • trimellitic anhydride monoacid chloride is preferred.
  • the comonomer comprises preferably at least one aromatic ring. Besides, it comprises preferably at most two aromatic rings. More preferably, the comonomer is a diamine. Still more preferably, the diamine is chosen from the group consisting of 4,4'-diaminodiphenylmethane, 4,4'-diaminodiphenylether, m-phenylenediamine and mixtures thereof.
  • the bearing assembly of the invention can possibly comprises at least one lubricating composition comprised within said outer race and said inner race.
  • Said lubricant can be used for enhancing mobility of rolling elements within the groove and/or as heat dissipation additive.
  • Preferred lubricating compositions suitable for the purposes of the invention are those comprising notably any of the following lubricants, possibly in combination with a thickener :
  • lubricants of this family generally comprise at least one oil (i.e. only one or a mixture of more than one oil) complying with either of formulae (I) and (II) here below : A-0[(CF(CF 3 )CF 2 0] n (CFX) m -A' (I)
  • X is F or CF 3
  • a and A' are selected from -CF 3 , -C 2 F 5 or -C 3 F 7 ;
  • n and n are independently integers >0, selected in such a way that m+n ranges from 8 to 55 and n/m ranges from 10 to 50; should n and m be both different from zero, the different recurring units are generally statistically distributed along the chain;
  • a and A' are as defined above and
  • p and q are independently integers >0, selected in such a way that p + q ranges from 35 to 220 and p/q ranges from 0.5 to 2.
  • these lubricants generally comprising at least one (i.e. one or mixtures of more than one) low-molecular weight, fluorine end-capped, homopolymer of hexafluoropropylene epoxide with the following chemical structure :
  • these lubricants generally comprising at least one (i.e. one or mixture of more than one oil complying with formula :
  • More preferred PFPE lubricants are FOMBLIN ® PFPEs complying with formula (II) as above detailed.
  • Suitable thickeners which can be used in the lubricant composition are notably polytetrafluoroethylene (PTFE) or inorganic compounds, e.g. talc.
  • PTFE polytetrafluoroethylene
  • talc inorganic compounds
  • Fomblin ® fluorinated fluids as base oils for high temperature, high performance greases is therefore one desirable option for filling the void between the inner and outer race(s).
  • Fomblin ® PFPE greases are derived by thickening Fomblin ® PFPE fluids with PTFE.
  • PFPEs may be added along with standard base oils, such as mineral and synthetic oils, to make stable greases containing conventional thickeners.
  • the bearing assembly of the invention can be used in a variety of fields. An initial and direct purpose has been to provide bearings for ailerons of aircrafts, including solar powered aircrafts, and even motor vehicle and heavy machinery equipment.
  • bearing assemblies of the invention are of particular interest in fields of use wherein weight reduction and functionality are of extreme importance, including in aircrafts, as every ounce of added weight increases energy consumption.
  • the bearing assembly of the invention have found application in the development notably of "Solar impulse" solar powered aircraft (htt ://www. so!arimpu!se .com/) .
  • FIG. 1 A a cross-sectional top or side view of a typical standard ball bearing having an inner race (IR) (110) and an outer race (OR) (120).
  • the inner race (110) has been concentrically placed within the outer race (120) so that the geometric center of the inner r allows for a certain number of rolling elements or balls (130) - (here represented by a single two-dimensional disk) to be inserted between the two races - the IR (110) and the OR (120) on both sides of a symmetrical plane.
  • FIG. 1 A a cross-sectional top or side view of a typical standard ball bearing having an inner race (IR) (110) and an outer race (OR) (120).
  • the inner race (110) has been concentrically placed within the outer race (120) so that the geometric center of the inner r allows for a certain number of rolling elements or balls (130) - (here represented by a single two-dimensional disk) to be inserted between the two races - the IR (110) and the OR (120) on
  • IB illustrates the fact that initially, the fabricated bearing of the present disclosure includes a different outer race (125) that has been tapered from a thicker end (from right to left) to a thinner end, resulting in the forming of a "wedge-like" taper.
  • the rolling elements or ball(s) (130) are no longer concentrically spaced within the IR (110) and modified OR (125), but instead there is some eccentricity of the shape of the spacing between both races. This eccentricity or skewing of the shape of the spacing is caused by deforming the modified OR as the spacing between the IR (110) and the modified OR (125) can be controlled by deforming the modified OR (125).
  • FIG. 2 is a more detailed schematic representation of one half of a cross- sectional top side or end view of the modified outer race (OR) (225) versus that of the conventional (OR) - (220). It is clear that the thickness (Tl) of one end is much greater than that of the other end (T2) providing a sort of cantilever ability for stretching or elongating the thinner end.
  • the elongation of the modified outer race (225) allows for temporarily increasing the number of rolling elements or balls (230) that can be inserted in the spacing between the IR and the modified OR (225).
  • FIG. 3 is a simple graphical representation of this "cantilever" effect discussed above showing how the thinner (OR) (325) is more elastic at the thinner end (326) versus that of the thicker end (327) and is also indicative of the fact that the thinner (OR) - (325) will have a reduced load bearing capability regarding deformation that can occur under a static or dynamic load.
  • FIG.4 illustrates how to overcome the issues associated with the schematic shown in FIG. 3, in that the thinner outer race (OR) - 435 - is reinforced by an external separate tapered element (410) with a thinner end Tl (412) and a thicker end T2 (414) that is known as a Morse tapered shape (410) such that the Morse tapered section (410) increases the thickness of the thinner outer race (435) to adjust the thickness of the thinner end of the outer race (432) and the thicker end of the outer race (434) to achieve a reinforced consistent and uniform thickness set of rolling elements are placed within said space created between both races.
  • the construct of the separate non-metallic Morse tapered element (410) has a thickness which is inversely proportionally tapered to match the modified outer race portion in that (Tl) is the thicker portion and (T2) is the thinner portion.
  • FIG.5 is a full cross-sectional view of a modified bearing (500) with a skewed, eccentric, "ovalized” outer race (510) that provides enough spacing between the inner race (520) and the outer race (510) so that additional rolling elements (530) can be added to the bearing.
  • FIG. 6 is a full cross-sectional view of a completed bearing assembly (600) with comparable strength and load bearing capacity to that of an unmodified bearing with an unmodified outer race.
  • the bearing assembly (600) illustrates how the tapered Morse shaped section (615) is fit to and bonded with the earlier tapered section of the outer race (OR) - 610).
  • the Morse tapered section (615) requires the use of a thin film, which in this specific instance includes the use of polymer PAI and NMP such that said Morse tapered element can be solvent bonded to the outer race (610) during the overlaying step.
  • Other bonding methods that can be utilized include laser or spin welding as well as the use of ultrasonic welding.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Rolling Contact Bearings (AREA)

Abstract

A bearing assembly (400) and method for assembling the bearing is described that includes at least one non-metallic two-part matching tapered outer race (410, 435) and an inner race with at least one set of rolling elements contained in the space between both races by positioning the inner race within the two-part tapered outer race with the goal of creating an enlarged space between both races that allows for an increased number of rolling elements to be inserted into the space. This larger space is created by providing a thickness of one section of the two-part matching tapered outer race that is greater along one portion of the outer race than the thickness along another portion of the same tapered outer race and allowing for deforming the outer race so that the outer race is less concentric and more assymetrically skewed with respect to both the inner race and the initially symmetrical bearing prior to finalizing the bearing assembly.

Description

Bearing assembly and method
CROSS-REFERENCE TO RELATED APPLICATIO
This application claims priority to European application No. 13306782.7 filed December 19, 2013, the whole content of this application being
incorporated herein by reference for all purposes
BACKGROUND
Devices which have moving components may utilize bearings to support loads during the translation of motion. Bearing assemblies are typically used for axial loads where 360° rotational movement is desired. In moderate to heavily loaded applications, ball bearing materials are typically alloy steels. Steel permits high mechanical loads, long life, and resistance to wear. A roller ball bearing typically consists of an inner race, an outer race, a set of ball bearings and a bearing cage. Steel bearing assemblies must be manufactured with little or no distortion of their components to avoid damage. This factor limits the number of balls that may be placed in the race, thus providing a limitation on the ultimate load bearing capability of the roller bearing assembly.
The life, performance, weight and costs associated with bearings are strongly influenced by the materials that are used in the bearing assembly. Metal ball bearings are constructed in such a way that all of the components are assembled in a 'static' manner. The inner race is put in place on a flat surface, an outer race is placed over the top or "on" the inner race, the races are offset or spread apart to allow clearance on one side so that all of the allotted rolling elements (normally balls) may be placed in-between the two races. A cage is placed over the group of ball bearings to provide and maintain equal spacing between the rolling elements.
Polymeric bearings are normally limited in their range of use based upon at least two factors; resilience or yield strength of the materials employed and the number of load bearing rolling elements (primarily balls) which may be incorporated for containment within the spacing between the two races.
Traditional metal alloy ball bearing assemblies involves placing an outer race (OR) over an inner race (IR), displacing the outer race to one side and then "filling" or "stuffing" the rolling elements (balls) within the space between the races. The ultimate number of balls that may be placed inside the two races is constrained by the characteristics of the materials used; they are 'rigid" meaning they contain less than (7 %) elongation and a compressive modulus of at least 4 MPa which prohibits distortions during the assembly process.
As the race 'fills-up' the last ball is inserted with a 'tight-fit' or with little margin for movement due to the rigidity of the entire aggregate of components. Excessive distortion will lead to brittle failure or permanent elongation deformation, so normally additional balls may not be added to the aggregate.
The number of balls or rolling elements which can be introduced is increased by providing an elastic deformation in either or both of the two rings or races. Addition of the number of rolling elements between the races for a bearing increases the ability to support load and reduce friction and wear both external and internal to the bearing.
In order to increase the number of balls or rolling elements which can be inserted between the two races (rings) of a ball bearing, it has been further suggested to apply a force on two diametrically opposed locations on the outer ring or the inner ring, or on both rings, when both rings have been eccentrically displaced. This is disclosed in U.S. Pat. No. 2,633,627, German patent application 2 104 063 and JP 2006-177 507. It has also been proposed to apply forces on four points, on the outer ring, as disclosed in JP 2004-068 985, or on three points at 120 degrees on the outer ring as disclosed in U.S. Pat.
No. 2,885,767 which also provides similar application of forces on the inner ring.
US application 2012/0047742 indicates a method for assembly of a roller bearing with the primary object of the invention being a new and improved method of assembling a rolling bearing by inserting an increased number of rolling elements between the outer and the inner rings of the rolling bearing. To accomplish this goal, a method for assembling a rolling bearing having an outer and an inner ring and at least one row of rolling elements there between, which comprises positioning the inner ring eccentrically within the outer ring so as to form a crescent shape space. By successively inserting a number of rolling elements in this space until all the rolling elements are contacting each other and two extreme rolling elements are contacting both the inner and the outer rings, the method is accomplished. The method also comprises elastic deformation of the outer ring by applying forces from outside to three points on the periphery of the outer ring. Such a method allows for insertion of a greater number of rolling elements in the crescent shape space left between the inner and outer rings in an eccentric position without exceeding the elastic limit of the material constituting the outer ring. By first verifying the deformation and taking into account the elastic limit of the material, it is possible to ascertain that the insertion of the supplemental rolling element will be possible without permanently deforming the outer ring.
The method can also be repeated after it has been ascertained that insertion of one supplemental rolling element can be made without permanently deforming the outer ring and/or the inner ring.
In such a way, it is possible to insert more than one supplemental rolling element if calculation has shown that such an insertion is possible without permanent deformation of the outer and/or inner ring.
The steps of determination of the value of forces to be applied and of verification that the deformation remains elastic can be repeated more than once. Each time a further theoretical position of the two extreme rolling elements can be tried, until the limit of the elastic deformation is reached.
The maximum number of supplemental rolling elements which can be inserted in the crescent shape space without exceeding the elastic limit can thus be determined precisely, before applying the forces and effectively inserting the maximum number of supplemental rolling elements in said space.
This method can be applied to any type of rolling bearing, for example to ball bearings where the rolling elements are balls or the method can be applied to rolling bearings where the rolling elements are cylindrical rollers which could be needle bearings. The rolling bearings may have more than one row of rolling elements.
Although this recent application discloses methods permitting reaching the limit of the maximum possible number of rolling elements to be inserted between the two rings of a (primarily) roller or rolling bearing, it does not describe the precise manner required for the provision of a non-metallic, preferably plastic or polymeric bearing that is lighter in weight than its metallic counterpart and also has the ability to provide nearly equivalent functionality by adding these rolling elements. One basis for establishing this invention is the need to create a new manufacturing method and technique which enables more load bearing rolling elements to become contained within the race(s) without the usual constraints of current manufacturing methods.
There remains a need for creating such a bearing which includes an increased number of rolling elements inserted in a non-metallic bearing assembly. SUMMARY OF THE INVENTION
The present application relates to both a bearing assembly and to a method for assembling a bearing.
Hence, the present invention provides for a bearing assembly comprising at least one, two-part non-metallic outer race, at least one inner race located within the two-part outer race having a groove along its circumferential portion, and a set of rolling elements housed between said inner race and said outer race, wherein said the two-part outer race has a first part inner section and a second part outer section,
wherein both said first part inner section and said second part outer section are made from a plastic material and have individually a Morse tapered shape having a proximal end portion and a distal end portion wherein the proximal end portion have a first thickness and the distal end portion having a second thickness different from thickness of proximal end portion; and
wherein said first part inner section and second part outer section are
geometrically opposed mirror shapes and assembled so as to ensure the overall thickness of the two-part outer race is consistent and uniform along its entire circumference.
Thanks to the particular design of the two-part non-metallic outer race, and in particular to the presence of thinner sections possessing increased deformation capabilities, it is advantageously possible to induce a deformation in said outer race, hence enabling insertion of a greater number of rolling elements without permanently deforming the outer ring and/or the inner ring.
As a consequence, the bearing assembly of the present invention advantageously includes a larger number of rolling elements (balls) in the expanded volumetric space between inner and outer races than might exist for a traditional metallic bearing assembly of substantially same shape.
The invention additionally provides for a method for assembling the bearing assembly as above described, said method comprising;
(i) forming said first part inner section having Morse tapered shape of said two- part non-metallic outer race from a plastic material;
(ii) forming an inner race portion and placing said inner race portion within said first inner section;
(iii) deforming said first part inner section by stretching the same to a value less than the elastic yield value or no greater than the elastic limit of the plastic material, thereby causing elongation of said first inner part section and skewing said first inner part section into a non-symmetrical shape that increases said space between both races;
(iv) placing a set of rolling elements within said space between both races;
(v) separately forming said second part outer section having Morse tapered
shape of said two-part non-metallic outer race from a plastic material,
(vi) overlaying and bonding said second outer part section onto said first inner part section, thereby creating a consistent and uniform thickness along the circumference of said outer race, thus providing a finished bearing assembly.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1A is a cross-sectional top or side view of a typical standard ball bearing having an inner race and an outer race.
FIG. IB is also a cross-sectional top or side view indicating the fabricated bearing of the present disclosure with a different outer race that has been tapered from a thicker end (from right to left) to a thinner end, resulting in the forming of a "wedge-like" taper. This taper is often referred to in the literature as a "Morse" taper.
FIG. 2 is a detailed schematic representation of one half of a cross- sectional top side or end view of the modified outer race (OR) versus that of the conventional (OR).
FIG. 3 is a simple graphical representation of the "cantilever" effect showing how the thinner (OR) is more elastic at the thinner end versus that of the thicker end.
FIG.4 illustrates how to overcome the issues associated with the schematic shown in FIG. 3, in that the thinner outer race (OR) is reinforced by an external separate tapered element with a thinner end Tl and a thicker end T2 that is known as a Morse tapered section such that the Morse tapered section increases the thickness of the thinner outer race.
FIG.5 is a full cross-sectional view of a modified bearing of one
embodiment of the present invention with a skewed, eccentric, "ovalized" outer race that provides enough spacing between the inner race and the outer race so that additional rolling elements can be added to the bearing.
FIG. 6 is a full cross-sectional view of a completed bearing assembly with comparable strength and load bearing capacity to that of an unmodified bearing with an unmodified outer race. DETAILED DESCRIPTION
The bearing assembly of the present invention generally has a symmetrical shape that is either spherical or cylindrical.
In the bearing assembly, said two-part outer race and optionally said inner race are formed from a plastic material.
In the bearing assembly of the present invention, said two-part outer race is generally capable of at least 7 percent elongation, and according to certain embodiments even of at least 16 percent elongation, without causing an increase in the permanent yield or exceeding the elastic limit of said two-part non- metallic outer race.
The Morse tapered shape of the said first part inner section and said second part outer section are advantageously as defined in ISO standard 296, which is hereby incorporated by reference.
The said first part inner section and said second part outer section having Morse tapered shape are assembled in the bearing assembly of the invention and overlaid and bonded in step (vi) of the method as above described so that at least outer surface of said first part inner section and inner surface of said second part outer section are placed in intimate contact with one another so that there is a capability to resist slipping, disassociation (breaking apart) and essentially forming a physically single structural or load bearing unit. To enhance the adhesion between these surfaces an additional adhesive system may be used to render a more homogeneous bonded structural support. This adhesive may be formulated using same plastic material which is the main constituent of said first part inner section and second part inner section. When the plastic material includes polymer (PAI) as polymer ingredient, it is advantageously possible to use as adhesive a composition obtained by mixing at least one polymer (PAI) in powder form with an organic solvent. One example of an acceptable solvent is NMP N-methyl pyrolidone - other solvents which at least partially solubilize polymer PAI can also be used. Other bonding techniques can be used to enhance the adhesion between outer surface of said first part inner section and inner surface of said second part outer section; these techniques may include laser or spin welding, ultrasonic bonding, etc.
The bearing assembly of the invention may additionally comprise an additional support ring which is circumferentially fixed on the outer surface of the two-part non-metallic outer race. This support ring can be machined, molded, formed or created in any suitable manner to fit with the outer surface of the two-part non-metallic outer race. This support ring is generally intended to provide additional structural integrity and cause the said two-part non-metallic outer race to no longer exhibit deformable characteristics and behavior either free from or under load.
The plastic material of said two-part outer race and optionally of said inner race of the bearing assembly of the invention generally comprises a polymer component as major constituent and optionally one or more than one additive.
The plastic material of the said first part inner section and of the said second part outer section of the two-part outer race can be the same material or can be a different material. Nevertheless, embodiments wherein both said first part inner section and said second part outer section of the two-part outer race are made from the same plastic material, as detailed below.
As polymer component of said plastic material, several polymers are known that can provide the necessary elongation and lubricity characteristics required. Among these are : polyetherarylketone polymers (PAEK), including PEEK, aromatic polyimide polymers, including aromatic polyamide-imide polymer [polymer (PAI)], polyphenylene polymers and blends thereof.
Said additive is generally a fibrous filler selected from the group consisting of carbon fibers, molybdynum disulfide, graphite, PI PE
(poiytetrafluoroethylene), glass fibers, organic fibers formed from high temperature engineered resins, and mixtures thereof. In alternative or in combination with the fibrous filler, one or more non-fibrous surface modifier selected from the group consisting of a liquid, a particulate surface modifier and mixtures thereof can be further used as additives.
The weight percentage of these additives are to be used in combination with the polymer component could be any percentage deemed necessary to improve the physical attributes of the bearing assembly such as reduced friction and wear, toughness, and lubricity.
Particularly advantageous results can be obtained when the plastic material comprises an aromatic polyamide-imide polymer [polymer (PAI)].
This polymer (PAI) exhibits sufficient elongation and compressive modulus that allows for the necessary distortion and elongation as necessary for manufacturing the bearing assembly, as above detailed, and yet possess the mechanical and lubricious properties which are required during 'normal' lifetime operations of the nearing assembly. The expression "aromatic polyamide-imide polymer [polymer (PAI)]" as used herein is intended to denote any polymer comprising more than 50 % moles of recurring units comprising at least one aromatic ring, at least one imide group, as such and/or in its amic acid form, and at least one amide group which is not included in the amic acid form of an imide group [recurring units (RPAI)] .
The recurring units (RPAI) are advantageously chosen among those of formula :
Figure imgf000009_0001
Wherein :
Ar is a trivalent aromatic group; typically Ar is selected from the group consisting of following structures :
Figure imgf000009_0002
and corresponding optionally substituted structures, with X being -0-, -C(O)-, -CH2-, -C(CH3)2-, -C(CF3)2-, -(CF2)q-, with q being an integer from 1 to 5 ; R is a divalent aromatic group; typically R is selected from the group consisting of following structures :
Figure imgf000009_0003
and corresponding optionally substituted structures, with Y being -0-, -S-, -SO2-, -CH2-, -C(O)-, -C(CH3)2-, -C(CF3)2-, -(CF2)q, q being an integer from 1 to 5.
Preferably, the aromatic polyamide-imide comprises more than 50 % of recurring units (RPAI) comprising an imide group in which the imide group is present as such, like in recurring units (RpAi-a), and/or in its amic acid form, like in recurring units (RpAi-b).
Recurring units (RPAI) are preferably chosen from recurring units (1), (m) and (n), in their amide-imide (a) or amide-amic acid (b) forms :
Figure imgf000010_0001
wherein the attachment of the two amide groups to the aromatic ring as shown in (1-b) will be understood to represent the 1,3 and the 1,4 polyamide-amic acid configurations ;
Figure imgf000010_0002
wherein the attachment of the two amide groups to the aromatic ring as shown in (m-b) will be understood to represent the 1 ,3 and the 1 ,4 polyamide-amic acid configurations ; and
Figure imgf000010_0003
n-Q
n-b
(amide-imide form)
(amide-amic acid form)
(n) wherein the attachment of the two amide groups to the aromatic ring as shown in (n-b) will be understood to represent the 1 ,3 and the 1 ,4 polyamide-amic acid configurations. More preferably, the polymer (PAI) comprises more than 90 % moles of recurring units (RPAI). Still more preferably, it contains no recurring unit other than recurring units (RPAI). Polymers commercialized by Solvay Specialty Polymers USA, L.L.C. as TORLON® polyamide-imides comply with this criterion.
Torlon® 4000T is an aromatic polyamide-imide polymer commercially available from Solvay Specialty Polymers USA, LLC.
The (PAI) polymer can be manufactured according to known methods in the art.
Processes for preparing (PAI) polymers are disclosed in detail, for example, in British Patent No. 1,056,564, U.S. Pat. No. 3,661,832 and U.S. Pat. No. 3,669,937.
For example, the (PAI) polymer can be notably manufactured by a process including the polycondensation reaction between at least one acid monomer chosen from trimellitic anhydride and trimellitic anhydride monoacid halides and at least one comonomer chosen from diamines and diisocyanates.
Among the trimellitic anhydride monoacid halides, trimellitic anhydride monoacid chloride is preferred.
The comonomer comprises preferably at least one aromatic ring. Besides, it comprises preferably at most two aromatic rings. More preferably, the comonomer is a diamine. Still more preferably, the diamine is chosen from the group consisting of 4,4'-diaminodiphenylmethane, 4,4'-diaminodiphenylether, m-phenylenediamine and mixtures thereof.
The bearing assembly of the invention can possibly comprises at least one lubricating composition comprised within said outer race and said inner race.
Said lubricant can be used for enhancing mobility of rolling elements within the groove and/or as heat dissipation additive.
Preferred lubricating compositions suitable for the purposes of the invention are those comprising notably any of the following lubricants, possibly in combination with a thickener :
- lubricants commercially available under the trade name FOMBLIN® (type Y, M, W, or Z) from Solvay Specialty Polymers Italy, S.p.A.; lubricants of this family generally comprise at least one oil (i.e. only one or a mixture of more than one oil) complying with either of formulae (I) and (II) here below : A-0[(CF(CF3)CF20]n(CFX)m-A' (I)
Wherein : X is F or CF3
A and A', equal to or different from one another, are selected from -CF3, -C2F5 or -C3F7;
m and n are independently integers >0, selected in such a way that m+n ranges from 8 to 55 and n/m ranges from 10 to 50; should n and m be both different from zero, the different recurring units are generally statistically distributed along the chain;
A-0-(C2F40)p(CF20)q-A' (II) Wherein :
A and A' are as defined above and
p and q are independently integers >0, selected in such a way that p + q ranges from 35 to 220 and p/q ranges from 0.5 to 2.
- lubricants commercially available under the trade name K YTOX® from Du
Pont de Nemours, these lubricants generally comprising at least one (i.e. one or mixtures of more than one) low-molecular weight, fluorine end-capped, homopolymer of hexafluoropropylene epoxide with the following chemical structure :
Figure imgf000012_0001
- lubricants commercially available under the trade name DEMNUM® from
Daikin, these lubricants generally comprising at least one (i.e. one or mixture of more than one oil complying with formula :
Figure imgf000012_0002
1=0 or integer > 0: n÷j = 10 to 153
More preferred PFPE lubricants are FOMBLIN® PFPEs complying with formula (II) as above detailed.
Suitable thickeners which can be used in the lubricant composition are notably polytetrafluoroethylene (PTFE) or inorganic compounds, e.g. talc.
The use of Fomblin® fluorinated fluids as base oils for high temperature, high performance greases is therefore one desirable option for filling the void between the inner and outer race(s). Fomblin® PFPE greases are derived by thickening Fomblin® PFPE fluids with PTFE. For Fomblin® PFPE-hybrid greases, PFPEs may be added along with standard base oils, such as mineral and synthetic oils, to make stable greases containing conventional thickeners. The bearing assembly of the invention can be used in a variety of fields. An initial and direct purpose has been to provide bearings for ailerons of aircrafts, including solar powered aircrafts, and even motor vehicle and heavy machinery equipment. More specifically, bearing assemblies of the invention are of particular interest in fields of use wherein weight reduction and functionality are of extreme importance, including in aircrafts, as every ounce of added weight increases energy consumption. The bearing assembly of the invention have found application in the development notably of "Solar impulse" solar powered aircraft (htt ://www. so!arimpu!se .com/) .
Reduction of weight with a degree of functionality that approaches that of metallic heavier weighted bearings, is not only useful in the aerospace industry, but reduction of fuel consumption is essential in the automotive, farm equipment, off-road vehicle, and trucking industries as well. Motorcycles, power tools, and sporting goods (such as bicycles, roller skates, roller blades, and essentially all automated machinery such as pitching machines, printers and copying machines, printing presses, etc.) all would benefit from these devices. In short, any rotatable device requiring metallic bearings could possibly be fitted alternatively with the at least partially non-metallic bearings described in the present disclosure. The determination for need would be made on a "case-by-case" basis determined primarily by load, friction reduction, and cost considerations.
Referring now more particularly to the drawings, there is shown
on FIG. 1 A a cross-sectional top or side view of a typical standard ball bearing having an inner race (IR) (110) and an outer race (OR) (120). The inner race (110) has been concentrically placed within the outer race (120) so that the geometric center of the inner r allows for a certain number of rolling elements or balls (130) - (here represented by a single two-dimensional disk) to be inserted between the two races - the IR (110) and the OR (120) on both sides of a symmetrical plane. FIG. IB illustrates the fact that initially, the fabricated bearing of the present disclosure includes a different outer race (125) that has been tapered from a thicker end (from right to left) to a thinner end, resulting in the forming of a "wedge-like" taper. Here the rolling elements or ball(s) (130) are no longer concentrically spaced within the IR (110) and modified OR (125), but instead there is some eccentricity of the shape of the spacing between both races. This eccentricity or skewing of the shape of the spacing is caused by deforming the modified OR as the spacing between the IR (110) and the modified OR (125) can be controlled by deforming the modified OR (125). This temporary deformation causes "ovalization" of the overall shape of the bearing (100) and is much simpler to achieve at the thin end of the OR (126) as opposed to that of the thicker end of the OR (127) by stretching or elongating this end (126) but being careful not to exceed the elastic limits or the yield strength or the actual yield point of the material of construction of the modified OR (125).
FIG. 2 is a more detailed schematic representation of one half of a cross- sectional top side or end view of the modified outer race (OR) (225) versus that of the conventional (OR) - (220). It is clear that the thickness (Tl) of one end is much greater than that of the other end (T2) providing a sort of cantilever ability for stretching or elongating the thinner end. The elongation of the modified outer race (225) allows for temporarily increasing the number of rolling elements or balls (230) that can be inserted in the spacing between the IR and the modified OR (225).
FIG. 3 is a simple graphical representation of this "cantilever" effect discussed above showing how the thinner (OR) (325) is more elastic at the thinner end (326) versus that of the thicker end (327) and is also indicative of the fact that the thinner (OR) - (325) will have a reduced load bearing capability regarding deformation that can occur under a static or dynamic load.
FIG.4 illustrates how to overcome the issues associated with the schematic shown in FIG. 3, in that the thinner outer race (OR) - 435 - is reinforced by an external separate tapered element (410) with a thinner end Tl (412) and a thicker end T2 (414) that is known as a Morse tapered shape (410) such that the Morse tapered section (410) increases the thickness of the thinner outer race (435) to adjust the thickness of the thinner end of the outer race (432) and the thicker end of the outer race (434) to achieve a reinforced consistent and uniform thickness set of rolling elements are placed within said space created between both races. The construct of the separate non-metallic Morse tapered element (410) has a thickness which is inversely proportionally tapered to match the modified outer race portion in that (Tl) is the thicker portion and (T2) is the thinner portion.
FIG.5 is a full cross-sectional view of a modified bearing (500) with a skewed, eccentric, "ovalized" outer race (510) that provides enough spacing between the inner race (520) and the outer race (510) so that additional rolling elements (530) can be added to the bearing.
FIG. 6 is a full cross-sectional view of a completed bearing assembly (600) with comparable strength and load bearing capacity to that of an unmodified bearing with an unmodified outer race. The bearing assembly (600) illustrates how the tapered Morse shaped section (615) is fit to and bonded with the earlier tapered section of the outer race (OR) - 610). The Morse tapered section (615) requires the use of a thin film, which in this specific instance includes the use of polymer PAI and NMP such that said Morse tapered element can be solvent bonded to the outer race (610) during the overlaying step. Other bonding methods that can be utilized include laser or spin welding as well as the use of ultrasonic welding.
Filling of the spacing between the inner (620) and outer (610) races with fluids that can assist in friction and wear reduction are also contemplated by the present invention.
Instead of having, for example the possibility of placing 10 or 12 balls within the spacing between the inner and outer race, it is now possible that more rolling elements (perhaps 11 or 13 or more bails) can be placed within the spacing and consequently higher load applications can be afforded. This allows for approaching the performance of metal bearing technology and provides for a lightweight alternative application with a longer life bearing than one with a lower set of rolling elements (less balls) design.
Should the disclosure of any patents, patent applications, and publications which are incorporated herein by reference conflict with the description of the present application to the extent that it may render a term unclear, the present description shall take precedence

Claims

C L A I M S
1. A bearing assembly comprising at least one, two-part non-metallic outer race, at least one inner race located within the two-part outer race having a groove along its circumferential portion, and a set of rolling elements housed between said inner race and said outer race, wherein the said two-part outer race has a first part inner section and a second part outer section, wherein both said first part inner section and said second part outer section are made from a plastic material and have individually a Morse tapered shape having a proximal end portion and a distal end portion wherein the proximal end portion has a first thickness and the distal end portion has a second thickness different from thickness of proximal end portion; and wherein said first part inner section and second part outer section are
geometrically opposed mirror shapes and assembled so as to ensure the overall thickness of the two-part outer race is consistent and uniform along its entire circumference .
2. The bearing assembly of claim 1, wherein said plastic material comprises a polymer component as major constituent and optionally one or more than one additive.
3. The bearing assembly of claim 2, wherein said polymer component is selected from the group consisting of polyetherarylketone polymers (PAEK), including PEEK, aromatic polyimide polymers, including aromatic polyamide- imide polymer [polymer (PAI)], polyphenylene polymers and blends thereof.
4. The bearing assembly of claim 3, wherein said polymer component is polymer (PAI).
5. The bearing assembly of anyone of claims 2 to 4, wherein said additive is a fibrous filler selected from the group consisting of carbon fibers,
molybdynum disulfide, graphite, PTFE (polytetrafluoroethylene), glass fibers, organic fibers formed from high temperature engineered resins, and mixtures thereof.
6. The bearing assembly of anyone of the preceding claims 1, wherein said bearing assembly is a symmetrical shape that is either spherical or cylindrical.
7. The bearing assembly of anyone of the preceding claims, wherein said two-part outer race is capable of at least 7 percent elongation without causing an increase in the permanent yield or exceeding the elastic limit of said two-part non-metallic outer race.
8. The bearing assembly of claim 7, wherein said percent elongation is at least 16 percent.
9. The bearing assembly of anyone of the preceding claims, said bearing assembly further comprising an additional support ring which is
circumferentially fixed on the outer surface of the two-part non-metallic outer race.
10. A method for assembling the bearing assembly according to anyone of claims 1 to 9, said method comprising;
(i) forming said first part inner section having Morse tapered shape of said two- part non-metallic outer race from a plastic material;
(ii) forming an inner race portion and placing said inner race portion within said first inner section;
(iii) deforming said first part inner section by stretching the same to a value less than the elastic yield value or no greater than the elastic limit of the plastic material, thereby causing elongation of said first inner part section and skewing said first inner part section into a non-symmetrical shape that increases said space between both races;
(iv) placing a set of rolling elements within said space between both races;
(v) separately forming said second part outer section having Morse tapered shape of said two-part non-metallic outer race from a plastic material,
(vi) overlaying and bonding said second outer part section onto said first inner part section, thereby creating a consistent and uniform thickness along the circumference of said outer race, thus providing a finished bearing assembly
11. The method of claim 10, wherein said first part inner section and said second part outer section having Morse tapered shape are overlaid and bonded in step (vi) so that at least outer surface of said first part inner section and inner surface of said second part outer section are placed in intimate contact with one another so that there is a capability to resist slipping, disassociation
(breaking apart) and essentially forming a physically single structural or load bearing unit.
12. The method of claim 11, wherein an additional adhesive is used to enhance the adhesion between said surfaces.
13. The method of claim 10, wherein said inner race is formed from a plastic material comprising a polymer component as major constituent and optionally one or more than one additive.
14. The method of claim 10, wherein said polymer component is an aromatic polyamide-imide polymer [polymer (PAI)].
15. The method of claim 10, wherein the final symmetrical shape of said bearing is either spherical or cylindrical.
PCT/EP2014/078086 2013-12-19 2014-12-16 Bearing assembly and method WO2015091569A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP14812546.1A EP3084242A1 (en) 2013-12-19 2014-12-16 Bearing assembly and method
US15/105,511 US20160312830A1 (en) 2013-12-19 2014-12-16 Bearing assembly and method

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP13306782.7 2013-12-19
EP13306782 2013-12-19

Publications (1)

Publication Number Publication Date
WO2015091569A1 true WO2015091569A1 (en) 2015-06-25

Family

ID=49998031

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2014/078086 WO2015091569A1 (en) 2013-12-19 2014-12-16 Bearing assembly and method

Country Status (3)

Country Link
US (1) US20160312830A1 (en)
EP (1) EP3084242A1 (en)
WO (1) WO2015091569A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107882886A (en) * 2017-11-03 2018-04-06 宁波慈兴智能设备有限公司 A kind of bearing full of complement balls aids in ball-loading device

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2565095B (en) * 2017-08-01 2020-03-11 Caterpillar Sarl Hitch assembly for articulated machines

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3224821A (en) * 1959-04-16 1965-12-21 Aircraft Armaments Inc Ball bearing

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US748825A (en) * 1904-01-05 Roller-bearing
US1600463A (en) * 1922-12-08 1926-09-21 Lewis C Feightner Roller bearing
FR2759129B1 (en) * 1997-01-31 1999-03-05 Roulements Soc Nouvelle BEARING AND BEARING COMPRISING A THERMAL COMPENSATION INSERT
JP2000240666A (en) * 1998-09-08 2000-09-05 Nsk Ltd Rolling bearing

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3224821A (en) * 1959-04-16 1965-12-21 Aircraft Armaments Inc Ball bearing

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107882886A (en) * 2017-11-03 2018-04-06 宁波慈兴智能设备有限公司 A kind of bearing full of complement balls aids in ball-loading device
CN107882886B (en) * 2017-11-03 2023-10-03 慈兴集团有限公司 Auxiliary ball loading device for full ball bearing

Also Published As

Publication number Publication date
US20160312830A1 (en) 2016-10-27
EP3084242A1 (en) 2016-10-26

Similar Documents

Publication Publication Date Title
WO2011040336A1 (en) Slide bearing
WO2013042715A1 (en) Sliding bearing and image formation device
CN109578438B (en) Sliding component
US10465750B2 (en) Sliding member, rolling bearing, and cage
US10082177B2 (en) Sliding engine component
JP2010054050A (en) Sliding structure combining two sliding members and sliding support device using the sliding structure
EP3084242A1 (en) Bearing assembly and method
US20190376559A1 (en) Sliding component, material and method
JP2015232382A (en) Cage for rolling bearing and rolling bearing
JP2009115128A (en) Retainer for roller bearing, and roller bearing
JP5342978B2 (en) Plain bearing
EP3315806A1 (en) Bearing material, bearing and method
JP5056394B2 (en) Roller bearing cage and rolling bearing
JP2008138815A (en) Rolling bearing and all rolling element bearing
EP3434919B1 (en) Holder for rolling bearing, and rolling bearing
JP2011127713A (en) Retainer for ball bearing, and ball bearing with the same
US9657781B2 (en) Robust touchdown bearing
JP2004076928A (en) Rolling bearing cage made of synthetic resin and rolling bearing
JP2017040275A (en) Radial spherical face slide bearing
WO2023027130A1 (en) Cage for rolling bearing and rolling bearing
JP2013113423A (en) Ball screw and injection molding machine
JP2006083965A (en) Rolling bearing
JP2020169653A (en) Slide member and slide bearing
CN107949711A (en) sliding component, rolling bearing and retainer
JP2006226180A (en) Swash plate of swash plate type compressor and swash plate type compressor

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 14812546

Country of ref document: EP

Kind code of ref document: A1

REEP Request for entry into the european phase

Ref document number: 2014812546

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2014812546

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 15105511

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE